WO2017107329A1 - 飞行滑板 - Google Patents

飞行滑板 Download PDF

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Publication number
WO2017107329A1
WO2017107329A1 PCT/CN2016/077295 CN2016077295W WO2017107329A1 WO 2017107329 A1 WO2017107329 A1 WO 2017107329A1 CN 2016077295 W CN2016077295 W CN 2016077295W WO 2017107329 A1 WO2017107329 A1 WO 2017107329A1
Authority
WO
WIPO (PCT)
Prior art keywords
power
foot
skateboard
flying
carrying
Prior art date
Application number
PCT/CN2016/077295
Other languages
English (en)
French (fr)
Inventor
陈乐春
Original Assignee
江苏数字鹰科技发展有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 江苏数字鹰科技发展有限公司 filed Critical 江苏数字鹰科技发展有限公司
Priority to US15/322,119 priority Critical patent/US10245500B2/en
Publication of WO2017107329A1 publication Critical patent/WO2017107329A1/zh

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Classifications

    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C17/00Roller skates; Skate-boards
    • A63C17/01Skateboards
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C17/00Roller skates; Skate-boards
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C17/00Roller skates; Skate-boards
    • A63C17/01Skateboards
    • A63C17/011Skateboards with steering mechanisms
    • A63C17/013Skateboards with steering mechanisms with parallelograms, follow up wheels or direct steering action
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C17/00Roller skates; Skate-boards
    • A63C17/12Roller skates; Skate-boards with driving mechanisms
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C17/00Roller skates; Skate-boards
    • A63C17/14Roller skates; Skate-boards with brakes, e.g. toe stoppers, freewheel roller clutches
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C17/00Roller skates; Skate-boards
    • A63C17/26Roller skates; Skate-boards with special auxiliary arrangements, e.g. illuminating, marking, or push-off devices
    • A63C17/267Roller skates; Skate-boards with special auxiliary arrangements, e.g. illuminating, marking, or push-off devices combined with wings or sails
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/04Initiating means actuated personally
    • B64C13/044Initiating means actuated personally operated by feet, e.g. pedals
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/16Initiating means actuated automatically, e.g. responsive to gust detectors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/20Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/026Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C17/00Roller skates; Skate-boards
    • A63C17/14Roller skates; Skate-boards with brakes, e.g. toe stoppers, freewheel roller clutches
    • A63C2017/1463Foot or toe operated
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C2203/00Special features of skates, skis, roller-skates, snowboards and courts
    • A63C2203/12Electrically powered or heated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use

Definitions

  • the present invention relates to the field of aircraft, and more particularly to a flying skateboard that can be applied to the fields of entertainment, transportation, and military.
  • Hendo Hover team in California has designed a magnetic levitation skateboard.
  • Hendo Hoverboarc This skateboard has four disc-shaped suspension engines at the bottom, which will generate special magnetic fields.
  • the ground is a metal plate, it generates a strong thrust and lifts the skateboard from the ground.
  • the principle is the same as that of a maglev train.
  • the present invention aims to provide a flying skateboard, which is truly a new entertainment product for young people through a reasonable power structure and free and precise control, and is popular all over the world, and can even be used in transportation and military fields.
  • a flight skateboard comprising:
  • the carrying portion includes a left foot carrying area and a right foot carrying area for carrying the left foot and the right foot of the human body; the left foot carrying area and the right foot carrying area are connected together and can be under the pedal of the human foot Relative rotation, so that the left foot bearing area and the right foot bearing area are on the same plane or on different planes, working in cooperation with the power part, so that the flight skateboard advances, retreats, brakes, shifts left and right, and turns left and right;
  • a power portion disposed on a circumference side of the carrying portion, for providing power for the moving motion of the flying skateboard;
  • a main control module including a gyroscope, mounted on the carrying portion, configured to control the power output of the power portion to maintain the balance of the flying skateboard, and to vertically or vertically hover or hover the flying skateboard;
  • the height sensing module is mounted on the carrying portion and has a built-in limited height threshold for measuring the distance between itself and the ground, and cooperates with the power unit to keep the flying height of the flying skateboard within the height limit threshold.
  • the left foot bearing area and the right foot bearing area are connected together and can be relatively rotated under the pedaling of the human foot, so that the left foot bearing area and the right foot bearing area are on the same plane or on different planes. .
  • the carrying portion when the carrying portion is tilted forward as a whole, the power portion is also inclined forward, and the flying slide is advanced; when the carrying portion is tilted rearward as a whole, the power portion is also inclined backward, and the flying skateboard is retracted or braked; The whole part is tilted to the left, the power part is also tilted to the left, and the flying slide is shifted to the left; when the carrying part is tilted to the right as a whole, the power part is also tilted to the right, and the flying slide is translated to the right.
  • the power portion connected to the left foot bearing region is also inclined backward with respect to the power portion connected to the right foot bearing region, and the flying skateboard is left.
  • the power portion connected to the left foot bearing region is also inclined forward with respect to the power portion connected to the right foot bearing region, and the flying skateboard is turned right;
  • the foot bearing area and the right foot bearing area are on the same plane, and the power part connected to the left foot bearing area is also in the same plane with respect to the power part connected to the right foot carrying area, and the flying skateboard does not turn.
  • the power unit includes a plurality of power sections, each power section is respectively connected to the carrier part, and each power section is balancedly arranged on the left foot bearing area and the right foot bearing area of the carrying part.
  • each power segment includes one or more power module groups arranged in an array, the power segment is covered with a cover plate, and the cover plate is respectively disposed above each power module group.
  • Airflow ventilation An airflow shield is respectively installed in each airflow ventilation of the cover plate.
  • the power module group is an internal combustion engine, an electric motor, a ducted engine, a jet engine or a rocket engine.
  • the left foot bearing area and the right foot bearing area are respectively mounted with sensors for sensing the actions of the left and right feet of the human body and the pressure applied to the flying skateboard.
  • the control method of the present invention can completely liberate people's hands and truly simulate the operation mode of the skateboard, so that people can experience the unique feeling of sliding and simulating surfing.
  • the invention makes up for the market vacancy, creates the fun of people to experience the air slide in the movement, and feels the charm and style of surfing, so that people can enjoy the body and mind and exercise the will.
  • the technology of the present invention can be used even in the fields of actual transportation and military.
  • FIG. 1 is a top plan view of the present invention.
  • FIG. 2 is a perspective view of the present invention.
  • 3 is a passenger state diagram of the present invention.
  • 5 is a left turn state diagram of the present invention.
  • FIG. 6 is a right turn state diagram of the present invention.
  • FIG. 7 is a view showing a module mounting position of the present invention.
  • FIG. 8 is a schematic diagram of the height-height height sensing of the present invention.
  • FIG. 1 and 2 are views of the present invention.
  • the flying skateboard of the present invention includes a carrying portion. 1 and the power unit 2.
  • the carrying portion 1 includes two bearing areas (shown in FIG. 2), which are: a left foot carrying area 3 and a right foot carrying area 4.
  • the human body stands on the carrying portion 1 (as shown in Fig. 3).
  • the left foot carrying area 3 is for carrying the left foot of the human body
  • the right foot carrying area 4 is for carrying the right foot of the human body.
  • the left foot bearing area 3 and the right foot bearing area 4 are connected together, and can be relatively rotated under the pedaling of the human foot, so that the left foot bearing area 3 and the right foot bearing area 4 are on the same plane or on different planes.
  • the power unit 2 is disposed on the circumference side of the carrying portion 1 for providing power for the moving motion of the flying skateboard.
  • the power unit 2 includes a plurality of power sections, each of which is connected to the carrier unit 1, and each power section is evenly arranged on the left foot bearing area 3 and the right foot bearing area 4 of the carrier unit 1.
  • the embodiment of Fig. 1 and Fig. 2 includes four power sections, two of which are arranged at the left front and the left rear of the left foot bearing area 3, and the other two are arranged at the right front and the right rear of the right foot carrying area 4.
  • each power section includes a plurality of power module groups 5 arranged in an array, the power module group 5 being an internal combustion engine, an electric motor, a ducted engine, a jet engine, or a rocket engine.
  • the power section is covered with a cover 6, and the cover 6 is respectively provided with airflow ventilation above each power module group 5, and an airflow shield 7 is installed in each airflow ventilation of the cover.
  • the movement direction of the flying skateboard of the present invention is controlled as follows:
  • the power portion 2 is also inclined rearward to generate a rearward force, and the flying skateboard is retracted or braked;
  • the power portion 2 When the carrying portion 1 is tilted to the right, the power portion 2 is also tilted to the right, generating a rightward force, and the flying slide is translated to the right.
  • the main control module 8 with reference to FIG. 7, is installed between the left foot carrying area 3 and the right foot carrying area 4 in this embodiment.
  • the main control module 8 uses existing flight controls, including gyroscopes, to separately control the power output of each power segment to maintain the balance of the flight skateboard and to cause the flight skateboard to move up and down vertically or hover in the air.
  • the height sensing module 9 with reference to Fig. 7, is mounted at the junction between the carrier portion 1 and the power portion 2 in this embodiment.
  • the height sensing module 9 has a built-in finite height threshold. As shown in Figure 8, the height sensing module 9 is capable of measuring its own distance from the ground and alerting the operator of the flying skateboard to ensure that the flying skateboard is at a safe height after the distance exceeds the height limit threshold.
  • the sensor 10 (shown in FIG. 2) is respectively mounted on the surfaces of the left foot bearing area 3 and the right foot bearing area 4, and the sensor 10 is configured to sense the motion of the left and right feet of the human body and the bearing
  • the pressure applied to the surface of the portion 1 sends the information to the main control module 8 for auxiliary control by the main control module 8.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Automation & Control Theory (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

一种飞行滑板,包括承载部(1)、动力部(2)、主控模块(8)、高度感应模块(9);承载部(1)包括左脚承载区域(3)和右脚承载区域(4),连接在一起并且可以在人体脚掌的踩踏下相对旋转,使左脚承载区域(3)和右脚承载区域(4)处于同一平面上或处于不同平面上,使飞行滑板前进、后退、刹车、左右平移、左右转向;主控模块(8)包括陀螺仪,用于控制动力部的功率输出来保持飞行滑板的平衡,以及使飞行滑板垂直上下运动或者悬停;高度感应模块(9)用于测量其自身与地面之间的距离,使飞行滑板的飞行高度保持在限高高度阈值内。该飞行滑板模拟滑板的操作方式,让人们体验空中滑行的乐趣。

Description

飞行滑板
技术领域
[0001] 本发明涉及飞行器领域, 更具体地, 涉及一种飞行滑板, 可应用于娱乐、 交通 及军事等领域。
背景技术
[0002] 据外媒报道, 美国加州的 Hendo Hover团队日前设计出一种磁悬浮滑板 Hendo Hoverboarc 这块滑板底部有 4个光盘形状的悬浮引擎, 会产生特殊的磁场。 当 地面是金属板的吋候, 它会产生强大的推力, 将滑板从地面举起来, 原理就跟 磁悬浮列车一样。
技术问题
[0003] 利用磁悬浮原理制造载人滑板理论上是可行的, 磁悬浮滑板的技术问题之一在 于供能方面, 要将人类体重带离地面几英尺并且还能平稳移动需要颇为巨大的 能量, 实际所需的能量和功率密度远超目前主流的锂离电池子所能提供的水平 。 事实确实如此, Hendo悬浮后大概离地 1英寸, 能承重 300磅。 但是这块磁悬浮 滑板需要花费 1万美元, 而且电池续航吋间只有 7分钟。
[0004] 另外采用磁悬浮技术的产品, 是由常温下的超导磁体提供驱动力的。 问题在于 像是磁浮列车这样的实际应用, 除了列车本身之外, 还需要超导轨道才能运转 起来。 而所谓的磁悬浮, 下方只有没有任何磁性的混凝土地面。 因此 Hendo最大 的缺点是, 它只能在非铁的金属表面实现悬浮, 所以没法随便把它带到家附近 的公园里玩。 而 Engadget报道称, Hendo在控制方向上也有一点问题。
问题的解决方案
技术解决方案
[0005] 本发明旨在提供一种飞行滑板, 通过合理的动力结构和自由、 精确的控制方式 , 使之真正成为年轻人的新式娱乐产品并且风靡全球, 甚至可用于交通运输及 军事领域。
[0006] 本发明的技术方案如下: [0007] 一种飞行滑板, 包括:
[0008] 承载部, 包括左脚承载区域和右脚承载区域, 用于承载人体的左脚和右脚; 所 述左脚承载区域和右脚承载区域连接在一起并且可以在人体脚掌的踩踏下相对 旋转, 使左脚承载区域和右脚承载区域处于同一平面上或处于不同平面上, 与 动力部协同工作, 使飞行滑板的前进、 后退、 刹车、 左右平移、 左右转向;
[0009] 动力部, 布置在承载部的周侧, 用于提供飞行滑板各向运动的动力;
[0010] 主控模块, 包括陀螺仪, 安装于承载部, 用于控制动力部的功率输出来保持飞 行滑板的平衡, 以及使飞行滑板垂直上下运动或者悬停;
[0011] 高度感应模块, 安装于承载部, 内置有限高高度阈值, 用于测量其自身与地面 之间的距离, 与动力部协同工作, 使飞行滑板的飞行高度保持在限高高度阈值 内。
[0012] 进一步的, 所述左脚承载区域和右脚承载区域连接在一起并且可以在人体脚掌 的踩踏下相对旋转, 使左脚承载区域和右脚承载区域处于同一平面上或处于不 同平面上。
[0013] 进一步的, 当承载部整体向前倾斜吋, 动力部也向前倾斜, 飞行滑板前进; 当 承载部整体向后倾斜吋, 动力部也向后倾斜, 飞行滑板后退或者刹车; 当承载 部整体向左倾斜吋, 动力部也向左倾斜, 飞行滑板向左平移; 当承载部整体向 右倾斜吋, 动力部也向右倾斜, 飞行滑板向右平移。
[0014] 进一步的, 当左脚承载区域相对于右脚承载区域向后转动吋, 与左脚承载区域 连接的动力部也相对于与右脚承载区域连接的动力部向后倾斜, 飞行滑板左转 ; 当左脚承载区域相对于右脚承载区域向前转动吋, 与左脚承载区域连接的动 力部也相对于与右脚承载区域连接的动力部向前倾斜, 飞行滑板右转; 当左脚 承载区域和右脚承载区域处于同一平面上吋, 与左脚承载区域连接的动力部也 相对于与右脚承载区域连接的动力部处于同一平面上, 飞行滑板不转向。
[0015] 进一步的, 所述动力部包括多个动力分部, 各动力分部分别与承载部相连, 且 各动力分部在承载部的左脚承载区域和右脚承载区域上呈均衡布置。
[0016] 进一步的, 每个动力分部包括以阵列形式布置的一个或多个动力模块组, 所述 动力分部上覆盖有盖板, 所述盖板于各动力模块组的上方分别设置有气流通气 , 在所述盖板的各个气流通气中分别安装有气流防护罩。
[0017] 进一步的, 所述动力模块组为内燃机、 电动机、 涵道式发动机、 喷气式发动机 或火箭式发动机。
[0018] 进一步的, 所述左脚承载区域和右脚承载区域表面分别安装有感应器, 所述感 应器用于感应人体左脚和右脚的动作以及对飞行滑板施加的压力。
发明的有益效果
有益效果
[0019] 本发明的有益技术效果是:
[0020] 本发明的控制方式可以完全解放人们的双手, 真实模拟滑板的操作方式, 让人 们体验滑行和模拟冲浪的独特感受。 本发明弥补了市场空缺, 创造了人们在运 动中体验空中滑行的乐趣, 又同吋感受到冲浪的魅力和风采, 使人们可以愉悦 身心, 锻炼意志。 本发明技术完善后甚至可用于实际的交通运输以及军事等领 域。
对附图的简要说明
附图说明
[0021] 图 1是本发明的顶面视图。
[0022] 图 2是本发明的立体视图。
[0023] 图 3是本发明的载人状态图。
[0024] 图 4是本发明的动力部分解图。
[0025] 图 5是本发明左转状态图。
[0026] 图 6是本发明右转状态图。
[0027] 图 7是本发明的模块安装位置图。
[0028] 图 8是本发明的限高高度感应示意图。
本发明的实施方式
[0029] 下面结合附图对本发明的具体实施方式做进一步说明。
[0030] 图 1、 图 2是本发明的视图。 如图 1、 图 2所示, 本发明的飞行滑板, 包括承载部 1与动力部 2。
[0031] 承载部 1包括两块承载区域 (如图 2所示) , 分别为: 左脚承载区域 3和右脚承 载区域 4。 人体站在承载部 1上 (如图 3所示) 吋, 左脚承载区域 3用于承载人体 的左脚, 右脚承载区域 4用于承载人体的右脚。 左脚承载区域 3和右脚承载区域 4 是连接在一起的, 并且可以在人体脚掌的踩踏下相对旋转, 可使得左脚承载区 域 3和右脚承载区域 4处于同一平面上或处于不同平面上。 动力部 2布置在承载部 1的周侧, 用于提供飞行滑板各向运动的动力。
[0032] 动力部 2包括多个动力分部, 各动力分部分别与承载部 1相连, 且各动力分部在 承载部 1的左脚承载区域 3和右脚承载区域 4上呈均衡布置。 图 1、 图 2的实施例中 包括 4个动力分部, 其中 2个布置在左脚承载区域 3的左前、 左后方, 另 2个布置 在右脚承载区域 4的右前、 右后方。
[0033] 图 4是本发明的动力部分解图。 如图 4所示, 每个动力分部包括以阵列形式布置 的多个动力模块组 5, 动力模块组 5为内燃机、 电动机、 涵道式发动机、 喷气式 发动机或火箭式发动机。 动力分部上覆盖有盖板 6, 盖板 6于各动力模块组 5的上 方分别设置有气流通气, 在盖板的各个气流通气中分别安装有气流防护罩 7。
[0034] 本发明飞行滑板的运动方向的控制方式如下:
[0035] 1、 前进、 后退、 刹车、 平移控制, 采用机械控制方式, 模拟地面滑板的控制 方式, 通过操作者脚部动作控制:
[0036] 当承载部 1向前倾斜吋, 动力部 2也向前倾斜, 产生向前的作用力, 飞行滑板前 进;
[0037] 当承载部 1向后倾斜吋, 动力部 2也向后倾斜, 产生向后的作用力, 飞行滑板后 退或者刹车;
[0038] 当承载部 1向左倾斜吋, 动力部 2也向左倾斜, 产生向左的作用力, 飞行滑板向 左平移;
[0039] 当承载部 1向右倾斜吋, 动力部 2也向右倾斜, 产生向右的作用力, 飞行滑板向 右平移。
[0040] 2、 转向控制, 采用机械控制方式, 通过操作者脚部动作控制:
[0041] 当左脚承载区域 3相对于右脚承载区域 4向后转动吋, 与左脚承载区域 3连接的 动力部也相对于与右脚承载区域 4连接的动力部向后倾斜, 产生左转向的作用力
, 飞行滑板左转, 如图 5所示;
[0042] 当左脚承载区域 3相对于右脚承载区域 4向前转动吋, 与左脚承载区域 3连接的 动力部也相对于与右脚承载区域 4连接的动力部向前倾斜, 产生右转向作用力, 飞行滑板右转, 如图 6所示;
[0043] 当左脚承载区域 3和右脚承载区域 4处于同一平面上吋, 与左脚承载区域 3连接 的动力部也相对于与右脚承载区域 4连接的动力部处于同一平面上, 不产生转向 作用力, 飞行滑板不转向。
[0044] 3、 高度控制, 采用现有飞控方式, 并辅以限高控制:
[0045] 主控模块 8, 参考图 7, 在此实施例中安装在左脚承载区域 3和右脚承载区域 4之 间。 主控模块 8采用现有的飞控, 包括陀螺仪, 能够分别控制各个动力分部的功 率输出, 从而保持飞行滑板的平衡, 以及使飞行滑板垂直上下运动或者悬停在 空中。
[0046] 高度感应模块 9, 参考图 7, 在此实施例中安装在承载部 1与动力部 2之间的连接 处。 高度感应模块 9内置有限高高度阈值。 如图 8所示, 高度感应模块 9能够测量 其自身与地面之间的距离, 并在距离超越限高高度阈值吋, 对飞行滑板的操作 者发出警报, 确保飞行滑板处于安全高度。
[0047] 可选择的, 在左脚承载区域 3和右脚承载区域 4表面分别安装感应器 10 (如图 2 所示) , 感应器 10用于感应人体左脚和右脚的动作以及对承载部 1表面所施加的 压力, 将这些信息送至主控模块 8, 通过主控模块 8进行辅助控制。
[0048] 以上所述的仅是本发明的优选实施方式, 本发明不限于以上实施例。 可以理解 , 本领域技术人员在不脱离本发明的精神和构思的前提下直接导出或联想到的 其他改进和变化, 均应认为包含在本发明的保护范围之内。

Claims

权利要求书
[权利要求 1] 一种飞行滑板, 其特征在于, 包括:
承载部, 包括左脚承载区域和右脚承载区域, 用于承载人体的左脚和 右脚; 所述左脚承载区域和右脚承载区域连接在一起并且可以在人体 脚掌的踩踏下相对旋转, 使左脚承载区域和右脚承载区域处于同一平 面上或处于不同平面上, 与动力部协同工作, 使飞行滑板的前进、 后 退、 刹车、 左右平移、 左右转向;
动力部, 布置在承载部的周侧, 用于提供飞行滑板各向运动的动力; 主控模块, 包括陀螺仪, 安装于承载部, 用于控制动力部的功率输出 来保持飞行滑板的平衡, 以及使飞行滑板垂直上下运动或者悬停; 高度感应模块, 安装于承载部, 内置有限高高度阈值, 用于测量其自 身与地面之间的距离, 与动力部协同工作, 使飞行滑板的飞行高度保 持在限高高度阈值内。
[权利要求 2] 根据权利要求 1所述的飞行滑板, 其特征在于: 所述左脚承载区域和 右脚承载区域连接在一起并且可以在人体脚掌的踩踏下相对旋转, 使 左脚承载区域和右脚承载区域处于同一平面上或处于不同平面上。
[权利要求 3] 根据权利要求 2所述的飞行滑板, 其特征在于: 当承载部整体向前倾 斜吋, 动力部也向前倾斜, 飞行滑板前进; 当承载部整体向后倾斜吋 , 动力部也向后倾斜, 飞行滑板后退或者刹车; 当承载部整体向左倾 斜吋, 动力部也向左倾斜, 飞行滑板向左平移; 当承载部整体向右倾 斜吋, 动力部也向右倾斜, 飞行滑板向右平移。
[权利要求 4] 根据权利要求 2所述的飞行滑板, 其特征在于: 当左脚承载区域相对 于右脚承载区域向后转动吋, 与左脚承载区域连接的动力部也相对于 与右脚承载区域连接的动力部向后倾斜, 飞行滑板左转; 当左脚承载 区域相对于右脚承载区域向前转动吋, 与左脚承载区域连接的动力部 也相对于与右脚承载区域连接的动力部向前倾斜, 飞行滑板右转; 当 左脚承载区域和右脚承载区域处于同一平面上吋, 与左脚承载区域连 接的动力部也相对于与右脚承载区域连接的动力部处于同一平面上, 飞行滑板不转向。
[权利要求 5] 根据权利要求 1〜4中任意一项所述的飞行滑板, 其特征在于: 所述动 力部包括多个动力分部, 各动力分部分别与承载部相连, 且各动力分 部在承载部的左脚承载区域和右脚承载区域上呈均衡布置。
[权利要求 6] 根据权利要求 5所述的飞行滑板, 其特征在于: 每个动力分部包括以 阵列形式布置的一个或多个动力模块组, 所述动力分部上覆盖有盖板 , 所述盖板于各动力模块组的上方分别设置有气流通气, 在所述盖板 的各个气流通气中分别安装有气流防护罩。
[权利要求 7] 根据权利要求 6所述的飞行滑板, 其特征在于: 所述动力模块组为内 燃机、 电动机、 涵道式发动机、 喷气式发动机或火箭式发动机。
[权利要求 8] 根据权利要求 1所述的飞行滑板, 其特征在于: 所述左脚承载区域和 右脚承载区域表面分别安装有感应器, 所述感应器用于感应人体左脚 和右脚的动作以及对飞行滑板施加的压力。
PCT/CN2016/077295 2015-12-22 2016-03-25 飞行滑板 WO2017107329A1 (zh)

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